SAE ARP 1281 : 2002
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR
Superseded date
29-02-2024
Superseded by
Published date
12-09-2002
Publisher
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1 Scope
1.1 Purpose
1.2 Product Classification
1.3 Field of Application
2 References
2.1 Applicable Documents
2.2 Definitions and Abbreviations
3 Technical Requirements
3.1 General
3.2 Design
3.3 Processes, Construction/Assembly Requirements
3.4 Performance
3.5 Installation/Maintenance Requirements
3.6 Documentation
4 Quality Assurance Provisions
4.1 General
4.2 Test Requirements
4.3 Classification of Tests
4.4 Test Procedures
4.5 Test Conditions
4.6 Acceptance Test Methods
4.7 Preproduction Test Methods
4.8 Qualification Test Methods
4.9 Test Reports, Design Changes and Approval Data
4.10 Preproduction and Qualification Test Failures
5 Preparation For Delivery
5.1 Preservation For Delivery
5.2 Packing
5.3 Marking of Shipment
6 Notes
Appendix A Technical Notes and Comments
Figure
Tables
This aerospace recommended practice provides a framework and suggested procedures or values for requirements for the design, performance, and test of hydraulically powered servoactuators for use in aircraft flight control systems.
| Committee |
A-6B1
|
| DocumentType |
Revision
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
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| MIL-STD-882 Revision E:2012 | System Safety |
| SAE AS6039D | Bearings, Ball, Rod End, Double Row, Self-Aligning |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| NASM33602:2011 | BOLTS, SELF-RETAINING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY, DESIGN AND USAGE REQUIREMENTS FOR |
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| MIL-PRF-22191 Revision F:2008 | Barrier Materials, Transparent, Flexible, Heat-Sealable |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
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| ASTM E 1444 : 2005 | Standard Practice for Magnetic Particle Testing |
| MS21343 Base Document:1971 | BOSS SPACING HYDRAULIC DESIGN STANDARD FOR |
| SAE AS 8775 : 1998 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR |
| SAE AS4088C | Aerospace Rod Scraper Gland Design Standard |
| MIL-STD-100 Revision G:1997 | ENGINEERING DRAWINGS |
| SAE AS1241D | Fire Resistant Phosphate Ester Hydraulic Fluid for Aircraft |
| MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
| MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
| SAE AS33649A | Bosses, Fluid Connection, Internal Straight Thread |
| NASM24665:2016 | PIN, COTTER (SPLIT) |
| SAE AMS2403M | Plating, Nickel General Purpose |
| SAE AMSF7190B | Forging, Steel, For Aircraft/Aerospace Equipment and Special Ordnance Applications |
| SAE AS1290B | Graphic Symbols for Aircraft Hydraulic and Pneumatic Systems |
| MIL-HDBK-838 Base Document:1997 | LUBRICATION OF MILITARY EQUIPMENT |
| SAE AS 4059F : 2013 | AEROSPACE FLUID POWER - CONTAMINATION CLASSIFICATION FOR HYDRAULIC FLUIDS |
| AN6204 Revision L:2013 | Valve, Hydraulic Bleeder |
| SAE ARP4386C | Terminology and Definitions for Aerospace Fluid Power, Actuation and Control Technologies |
| MIL-STD-1839 Revision D:2010 | STANDARD PRACTICE CALIBRATION AND MEASUREMENT REQUIREMENTS |
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| MIL C 26482 : G | CONNECTOR, ELECTRICAL (CIRCULAR, MINIATURE, QUICK DISCONNECT, ENVIRONMENT RESISTING) RECEPTACLES AND PLUGS, GENERAL SPECIFICATION FOR |
| MIL-HDBK-470 Revision A:1997 | Designing and Developing Maintainable Products and Systems, Volume I |
| SAE AS4941B | Aerospace - General Requirements for Commercial Aircraft Hydraulic Components |
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| NASM21224:2014 | NUT, SELF-LOCKING, CASTELLATED, HEXAGON, COUNTERBORED, ASSEMBLED WASHER, 250 DEGREES F, NON-METALLIC INSERT (FOR SELF-RETAINING BOLTS) |
| NASM15981:2010 | FASTENERS, EXTERNALLY THREADED, SELF-LOCKING DESIGN AND USAGE LIMITATIONS FOR |
| ASTM B 381 : 2013 : REDLINE | SPECIFICATION FOR TITANIUM AND TITANIUM ALLOY FORGINGS |
| MIL-C-11796 Revision C:1986 | CORROSION PREVENTIVE COMPOUND, PETROLATUM, HOT APPLICATION |
| SAE ARP490F | Electrohydraulic Servovalves |
| JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
| MIL-PRF-8805 Revision G:2016 | SWITCHES AND SWITCH ASSEMBLIES, SENSITIVE, SNAP ACTION (BASIC, LIMIT, PUSH BUTTON AND TOGGLE SWITCHES), GENERAL SPECIFICATION FOR |
| A-A-1898 Revision D:2012 | CUSHIONING MATERIAL, CELLULOSIC, PACKAGING |
| SAE AIR4922A | Primary Flight Control Hydraulic Actuation System Interface Definition |
| SAE AIR4066C | Aerospace Fluid Power – Materials and Characteristics of Flight Control Servoactuators of Various Aircraft |
| NAS847:2012 | CAPS AND PLUGS, PROTECTIVE, DUST AND MOISTURE SEAL |
| MIL-STD-961 Revision E:2003 | DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT |
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